US11434556B2ActiveUtilityA1
Austenitic alloys for turbochargers
Est. expiryOct 12, 2038(~12.3 yrs left)· nominal 20-yr term from priority
F05D 2300/123C22C 38/42C22C 38/46C22C 38/58C22C 38/02F05D 2300/132F05D 2220/40C21D 6/004C22C 38/34C21D 6/005C21D 9/0062C22C 38/44F05D 2300/171C22C 38/001C21D 2211/001C22C 38/005C22C 38/32Y02T10/12C22C 38/54F02M 26/04C22C 38/60C22C 38/48F01D 25/24F05D 2300/131C21D 1/18
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Claims
Abstract
The present disclosure relates to a novel iron-based austenitic alloy for a turbocharger housing and to methods of its preparation.
Claims
exact text as granted — not AI-modifiedThe invention claimed is:
1. A turbocharger housing for an internal combustion engine comprising an iron-based austenitic alloy, wherein the iron-based austenitic alloy consists of the following composition:
C: 0.3 to 0.45 wt. %,
Cr: 20 to 22 wt. %,
Mn: 9.5 to 11.5 wt. %,
Ni: 3 to 4 wt. %,
Si: 1.2 to 2.1 wt. %,
Nb: 0.4 to 0.6 wt. %,
V: 0.3 to 0.6 wt. %,
Mo: 0.3 to 0.6 wt. %,
N: 0.1 to 0.35 wt. %;
impurities in a total amount of less than 3 wt. %; and
Fe as balance;
wherein the turbocharger housing is cast from the iron-based austenitic alloy and wherein the iron-based austenitic alloy has a melting temperature of less than 1550° C.
2. The turbocharger housing according to claim 1 , wherein the iron-based austenitic alloy has a melting temperature in the range of 1450° C. to less than 1550° C.
3. The turbocharger housing according to claim 1 , wherein the iron-based austenitic alloy has less than 4% sigma phases.
4. The turbocharger housing according to claim 1 , wherein the iron-based austenitic alloy has less than 2% sigma phases.
5. The turbocharger housing according to claim 1 , wherein the microstructure of the iron-based austenitic alloy has an average grain size of between 2 and 4, measured according to ASTM E112-12.
6. The turbocharger housing according to claim 1 , wherein an inner surface of the turbocharger housing that is in contact with exhaust gas or compressed air has a surface roughness Rz of less than 100.
7. A process for preparing a turbocharger housing as defined in claim 1 , comprising
a) melt mixing elements of the following composition, wherein the composition consists of:
C: 0.3 to 0.45 wt. %,
Cr: 20 to 22 wt. %,
Mn: 9.5 to 11.5 wt. %,
Ni: 3 to 4 wt. %,
Si: 1.2 to 2.1 wt. %,
Nb: 0.4 to 0.6 wt. %,
V: 0.3 to 0.6 wt. %,
Mo: 0.3 to 0.6 wt. %;
N: 0.1 to 0.35 wt. %;
impurities in a total amount of less than 3 wt. %; and
Fe as balance, to form an iron-based austenitic alloy melt;
b) casting the melt into a turbocharger housing.
8. The process according to claim 7 , wherein the turbocharger housing is subjected to thermal aging at 1000° C. to 1060° C. for at least 1 hour, followed by cooling at a rate of up to 80° C./h.
9. The process according to claim 7 , wherein casting is an investment casting or a sand casting process.Cited by (0)
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